Computer Testing Supplement for IA.indb - Aviation Supplies ...

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Models 210K/210L/T210K/T210L (cont’d)
C.G. Range (Landing (+42.5) to (+53.0) at 3800 lb.
Gear Extended) (+37.0) to (+53.0) at 3000 lb. or less
Straight line variation between points given.
Moment change due to retracting landing gear (+3207 in.-lb.)
Empty Wt. C.G. Range None
*Maximum Weight 3800 lb.
No. of Seats Standard 6 (2 at +34 to +46, 2 at +61 to +77, 2 at +101)
Optional 4 (2 at +34 to +46, 2 at +77) (210K/T210K)
Maximum Baggage Reference weight and balance data
Fuel Capacity 90 gal. (89 gal. usable); two 45.0 gal. tanks in wings at +43
See NOTE 1 for data on unusable fuel.
Oil Capacity 10 qt. (-12.5); 8 qt. usable
See NOTE 1 for data on undrainable oil.
Control Surface Wing flaps Up 0° Down 30° +1°, -2°
Movements Ailerons Up 20° ±2° Down 15° ±2°
Elevator Up 23° ±1° Down 17° ±1°
Elevator tab Up 25° ±1° Down 10° ±1°
Rudder Right 24° ±1° Left 24° ±1°
(measured parallel to 0.0 W.L.)
Rudder Right 27°13' ±1° Left 27°13' ±1°
(measured perpendicular to hinge line)
Serial Nos. Eligible Models 210K/T210K: 21059200 through 21059351 (1970 Model)
21059352 through 21059502 (1971 Model)
Models 210L/T210L: 21059503 through 21059719 (1972 Model)
21059720 through 21060089 (1973 Model)
21060090 through 21060539 1974 Model)
21060540 through 21061039 1975 Model)
21061040 through 21061041 1976 Model)
21061043 through 21061573 (1976 Model)
XIV - Model 210M/T210M, 6 PCLM (Normal Category), October 7, 1976
Model 210M
Engine Continental IO-520-L
*Fuel Model 210M (S/N 21061574 through 21062273)
100/130 minimum grade aviation gasoline
Model 210M (S/N 21062274 through 21062953)
100LL/100 minimum grade aviation gasoline
*Engine Limits Takeoff (5 min.) at 2850 r.p.m. (300 hp.)
For all other operations, 2700 r.p.m. (285 hp.)